View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 57666U 26144.75290505 +.00000000 +00000-0 +86804-3 0 00002
2 57666 53.1605 274.9339 0000676 41.4155 318.6898 15.32464099 04
| Epoch (UTC): | 24 May 2026 18:04:10 |
| Eccentricity: | 0.0000676 |
| inclination: | 53.1605° |
| perigee height: | 468 km |
| apogee height: | 469 km |
| right ascension of ascending node: | 274.9339° |
| argument of perigee: | 41.4155° |
| revolutions per day: | 15.32464099 |
| mean anomaly at epoch: | 318.6898° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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